High-Frequency Combustion Instabilities in Liquid Rocket Engines Driven by Propellants Flow Rate Oscillations
Author(s) -
Robin Nez,
Thomas Schmitt,
Sébastien Ducruix
Publication year - 2018
Publication title -
hal (le centre pour la communication scientifique directe)
Language(s) - English
Resource type - Conference proceedings
Subject(s) - liquid propellant rocket , propellant , mechanics , coaxial , combustion , rocket engine , rocket (weapon) , large eddy simulation , combustion chamber , volumetric flow rate , flow (mathematics) , vortex , aerospace engineering , materials science , physics , chemistry , mechanical engineering , engineering , turbulence , organic chemistry
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